Ensuring the stability and control of the aircraft at critical angles of attack
Journal Title: Інформаційні системи, механіка та керування - Year 2015, Vol 0, Issue 13
Abstract
The aim of this paper is to study the effect of different combinations of structural funds management boundary layer of air on the aerodynamic characteristics of the aircraft, the development of guidelines for the selection of the most successful combination of sagging, vortex, vortex generators, as well as the geometric shape, size, location of the selected funds. To conduct the study were considered layout of the aircraft 'wing + fuselage "burly and turbulence; burly and vortex generators. Scientific novelty lies in the combination of the existing structural funds management boundary layer of air (sagging, vortex, vortex generators) to ensure the best aerodynamic characteristics and parameters of stability and controllability. This article describes the panel and the vortex method of calculating the aerodynamic aircraft required to perform research and development guidelines. Examining the results of calculations, we can say that the most successful combination is a combination of sagging and vortex generators. It can significantly increase the load-bearing properties of the aircraft, especially at the critical angles of attack, the critical angle of attack, as well as the effectiveness of the cross-government. The developed guidelines can be used for any purpose aircraft, of any size.
Authors and Affiliations
Олексій Анатолійович Волинець, Дмитро Миколайович Зінченко
Keywords
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- EP ID EP542733
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